| findByName(List, String) |   | 90% | | 75% | 1 | 3 | 1 | 5 | 0 | 1 |
| acceleration(FieldSpacecraftState, CalculusFieldElement[]) | | 100% | | 100% | 0 | 3 | 0 | 12 | 0 | 1 |
| extractParameters(CalculusFieldElement[], FieldAbsoluteDate) | | 100% | | 100% | 0 | 4 | 0 | 11 | 0 | 1 |
| extractParameters(double[], AbsoluteDate) | | 100% | | 100% | 0 | 4 | 0 | 11 | 0 | 1 |
| changeDragParameterDriversNames(DragSensitive, AbsoluteDate, String) | | 100% | | 87% | 1 | 5 | 0 | 8 | 0 | 1 |
| acceleration(SpacecraftState, double[]) | | 100% | | n/a | 0 | 1 | 0 | 8 | 0 | 1 |
| getParametersDrivers() | | 100% | | 83% | 1 | 4 | 0 | 7 | 0 | 1 |
| getFieldEventDetectors(Field) | | 100% | | 100% | 0 | 2 | 0 | 8 | 0 | 1 |
| getEventDetectors() | | 100% | | 100% | 0 | 2 | 0 | 7 | 0 | 1 |
| getTransitionDates() | | 100% | | 100% | 0 | 2 | 0 | 4 | 0 | 1 |
| TimeSpanDragForce(Atmosphere, DragSensitive) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| TimeSpanDragForce(Atmosphere, DragSensitive, TimeScale) | | 100% | | n/a | 0 | 1 | 0 | 5 | 0 | 1 |
| addDragSensitiveValidBefore(DragSensitive, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| addDragSensitiveValidAfter(DragSensitive, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 2 | 0 | 1 |
| getDragSensitive(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| extractDragSensitiveRange(AbsoluteDate, AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getDragSensitiveSpan(AbsoluteDate) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| getFirstSpan() | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| lambda$getFieldEventDetectors$1(FieldSpacecraftState, FieldEventDetector, boolean) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |
| lambda$getEventDetectors$0(SpacecraftState, EventDetector, boolean) | | 100% | | n/a | 0 | 1 | 0 | 1 | 0 | 1 |